P/N: 25-8te1-1a
Category: Flight Controls
This product requires a custom quote. Please contact our sales team for pricing information or submit an RFQ (Request for Quote).
| Condition | Stock |
|---|---|
| As Removed | 2 Available |
The 25-8te1-1a is a left-hand elevator assembly for aircraft pitch control. This primary flight-control surface attaches to the horizontal stabilizer via existing hinges and control linkages. Aluminum construction with riveted skin and internal reinforcement provides structural rigidity during flight operations.
The assembly connects to the control column through push-pull rods or cable systems, translating pilot input into pitch movements. Installation requires verification against the aircraft's Illustrated Parts Catalog and rigging per the Aircraft Maintenance Manual to ensure proper control authority and neutral positioning.
Please note: Product descriptions are provided for informational purposes. Always refer to your aircraft's Illustrated Parts Catalog (IPC) to verify part compatibility and specifications.
The 25-8te1-1a is a left-hand elevator assembly for aircraft pitch control. This primary flight-control surface attaches to the horizontal stabilizer via existing hinges and control linkages.
The ELEVATOR ASSEMBLY LH may be available as an OEM (Original Equipment Manufacturer) or PMA (Parts Manufacturer Approval) part depending on condition and source. Both carry FAA certification for airworthiness. Currently available in: As Removed. Contact us for sourcing details.
Installation hardware requirements vary by application. Check your aircraft's Structural Repair Manual (SRM) or Illustrated Parts Catalog (IPC) for the complete installation kit requirements for the ELEVATOR ASSEMBLY LH. We stock related hardware and can help identify companion parts.
Yes, we ship airframe components worldwide. International orders typically arrive within 3-14 business days depending on destination. Export documentation and customs forms are included. Contact us for international shipping quotes on the 25-8te1-1a.